Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Wisnoe, Wirachman"'
Autor:
Shukri, Ehan Sabah, Wisnoe, Wirachman
Publikováno v:
In Energy Procedia January 2019 156:249-253
Autor:
Wisnoe, Wirachman, Rahman, Khairil Muhaimin Abd, Istihat, Yusman, Natarajan, Valliyappan David
Publikováno v:
In Procedia Technology 2016 26:544-551
Autor:
Mohd Saad Nornashiha, Wisnoe Wirachman, Mohd Nasir Rizal Effendy, Mohd Ali Zurriati, Askari Ehan Sabah Shukri
Publikováno v:
MATEC Web of Conferences, Vol 256, p 02004 (2019)
This paper presents an aerodynamic characteristic study in longitudinal direction of UiTM Blended Wing Body-Unmanned Aerial Vehicle Prototype (BWB-UAV Prototype) equipped with horizontal stabilizers. Flight tests have been conducted and as the result
Externí odkaz:
https://doaj.org/article/77c3bc74081e43c0b511450962018cf5
Publikováno v:
MATEC Web of Conferences, Vol 95, p 07019 (2017)
In this study, acoustic analysis and thermofluid performance of a Ranque-Hilsch Vortex Tube (RHVT) is experimentally investigated under different orifice diameters at its cold tube. The orifice diameters used are 2mm, 3 mm, 4 mm, 5 mm and 6 mm. The i
Externí odkaz:
https://doaj.org/article/bdc29f438d0a4cb6967ed14537a8952a
Publikováno v:
Journal of Mechanical Engineering (1823-5514); 4/15/2021, Vol. 18 Issue 2, p125-144, 20p
Publikováno v:
Applied Mechanics and Materials. :582-586
Heat distribution and flow behaviors in an annular diffuser with twisted rectangular hub have been numerically simulated in the present work. The study is conducted with three different twist ratios (Y/W = 2.3, 1.5, and 1.16) for Reynolds number 2.5
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b5d74439d89584b81c8aefb60ecf134
https://doi.org/10.4028/www.scientific.net/amm.465-466.582
https://doi.org/10.4028/www.scientific.net/amm.465-466.582
Publikováno v:
Applied Mechanics and Materials. :515-519
In this experiment, the cold mass fraction, cold temperature difference and isentropic efficiency of Ranque-Hilsch Vortex Tube were investigated and measured. Three different inlet pressures (absolute) (296633 Pa, 394699.5 Pa and 492766 Pa) and 2 typ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::55edc6e466cd3e153f35236c0a0a9927
https://doi.org/10.4028/www.scientific.net/amm.465-466.515
https://doi.org/10.4028/www.scientific.net/amm.465-466.515
Publikováno v:
Applied Mechanics and Materials. 393:735-740
A heat pipe is a heat-transfer device that use the principles of thermal conductivity and phase change to transfer heat between two ends at almost constant temperature. The thermal peformance of cylindrical heat pipes depends on design parameters suc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b39d82c4c6961702ab0a828c145621e0
https://doi.org/10.4028/www.scientific.net/amm.393.735
https://doi.org/10.4028/www.scientific.net/amm.393.735
Publikováno v:
Advanced Materials Research. :584-588
This paper presents a study about split drag flaps as control surfaces to generate yawing motion of a blended wing body aircraft. These flaps are attached on UiTM’s Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) Baseline-II E-4. Deflection o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d8dd735227cfde5ef65177af84d1e7a
https://doi.org/10.4028/www.scientific.net/amr.433-440.584
https://doi.org/10.4028/www.scientific.net/amr.433-440.584
Publikováno v:
Advanced Materials Research. :6636-6640
The objective of this paper is to investigate longitudinal flight dynamics of the said aircraft at loitering flight condition near sea level. Three mathematical dynamic models are used to compute transient response of Baseline-II E-2 BWB along with a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e9b2bc3353d33c1bab990e59003267ee
https://doi.org/10.4028/www.scientific.net/amr.433-440.6636
https://doi.org/10.4028/www.scientific.net/amr.433-440.6636